TECHNICAL FIELD
[0001] The present invention relates to a surface-coated cutting tool, particularly a surface-coated
cutting tool covered with a coat film for improving wear resistance and chipping resistance.
BACKGROUND ART
[0002] For cutting tools, cemented carbide (WC-Co alloy, or the same having carbon nitride
such as Ti (titanium), Ta (tantalum), or Nb (niobium) added to) has been conventionally
used. However, in accordance with the trend of high speed cutting in the recent years,
cutting tools covered with at least one layer of a coat by using cemented carbide,
cermet, sintered cubic boron nitride, or alumina type or silicon nitride type ceramic
as the base material, and applying chemical vapor deposition (CVD) or physical vapor
deposition (PVD) on the surface has become pervasive. The coat layer has a thickness
of 3-20 µm, and is formed of a compound including a first element of at least one
type selected from the IVa group element, Va group element, VIa group element from
the periodic table of elements, Al (aluminum), Si or B, and a second element of at
least one type selected from B, C, N or O (when the first element is B alone, the
second element excludes B).
[0003] The demand for saving energy and reducing the cost in modern cutting machinery is
high. Accordingly, the demand for further increase in speed and feeding, as well as
high efficiency in machining is elevating in terms of the cutting machining conditions.
Further, the trend is towards low cost, high strength, and lightness in the machine
components. The workpiece material employed in components has become difficult to
be cut, rendering difficulty in the machining of the workpiece material. In view of
the foregoing, various approaches have been taken to increase the chipping resistance
and lifetime of cutting tools.
[0004] As an approach directed to increasing the lifetime of a cutting tool, Japanese Patent
Laying-Open No.
2001-062603 (Japanese Patent No.
3661503, Patent Literature 1), for example, discloses a coat film of an oblong crystal texture,
having residual stress differing between the upper section and lower section of the
coat film. Specifically, residual compressive stress is applied to the upper layer
of the coat film while residual tensile stress is applied to the lower layer of the
coat film, whereby the chipping resistance of the cutting tool is improved.
[0005] Japanese Patent Laying-Open No.
2001-096404 (Patent Literature 2) discloses the approach of improving chipping resistance by
covering with a hard coat layer including the stack of a Ti compound layer, a titanium
carbonitride layer, a titanium carbide layer, and an aluminum oxide layer.
[0006] Japanese Patent Laying-Open No.
2009-078309 (Patent Literature 3) teaches improving the chipping resistance by introducing compressive
stress towards the outer layer side of a hard coat layer covering the surface of a
surface-coated cutting tool by means of blasting.
[0007] Further,
WO2006/064724 (Patent Literature 4) discloses a coat film including a first coat formed of α-Al
2O
3 to which compressive stress is applied at the surface side and a second coat formed
of TiCN to which tensile stress is applied at the inner side. This coat film has the
toughness and wear resistance improved by setting the tensile stress of the first
coat and the compressive stress of the second coat to satisfy a predetermined relationship.
CITATION LIST
PATENT LITERATURE
SUMMARY OF INVENTION
TECHNICAL PROBLEM
[0009] Although sufficient performance in the chipping resistance can be achieved by the
approach disclosed in the aforementioned Patent Literatures 1- 4, the wear resistance
was not sufficient to satisfy the demand for current cutting tools.
[0010] In view of the foregoing, an object of the present invention is to provide a surface-coated
cutting tool with both wear resistance and chipping resistance highly established.
SOLUTION TO PROBLEM
[0011] As a result of diligent study to solve the problems set forth above, the inventors
of the present invention arrived at the finding that differentiating the crystal texture
of the chamfer portion of the coat film from the crystal texture of another portion
of the coat film other than the chamfer portion and applying different residual stress
to respective crystal textures are most effective for highly establishing both wear
resistance and chipping resistance. By further research based on this finding, the
inventors came to complete the present invention.
[0012] A surface-coated cutting tool of the present invention includes a base material,
and a coat film formed on the base material. The surface-coated cutting tool has a
chamfer portion where a rake face and a flank face meet. The coat film includes at
least one layer of a first coat layer. The first coat layer is the outermost surface
layer of the coat film at the chamfer portion. The first coat layer at the chamfer
portion has residual stress that exhibits a minimal value at a depth A within 2 µm
from the surface, and that increases continuously or stepwise as a function of depth
in a further depth direction from said depth A. The minimal value of the residual
stress is greater than or equal to -7 GPa and less than or equal to -1 GPa. The first
coat layer at a portion other than the chamfer portion has residual stress greater
than the minimal value of the residual stress, and that increases continuously or
stepwise as a function of advance in the central direction of the rake face and the
central direction of the flank face. The residual stress of the first coat layer other
than the chamfer portion is greater than or equal to 0 GPa and less than or equal
to 2 GPa at the base material side. In the first coat layer of the chamfer portion,
the region from the surface up to depth A is a fine crystal texture region including
crystals having an average grain size greater than or equal to 10 nm and less than
or equal to 200 nm. In the first coat layer, the region further in the depth direction
from depth A at the chamfer portion and the region other than the chamfer portion
is a rough crystal texture region including crystals larger than the crystal in the
fine crystal texture region.
[0013] The first coat layer preferably has a thickness greater than or equal to 2 µm and
less than or equal to 30 µm. Although the first coat layer is preferably the outermost
surface layer also at other regions in addition to the chamfer portion, the first
coat layer does not necessarily have to be the outermost surface layer.
[0014] The coat film is preferably formed of a compound including at least one type of element
selected from the group consisting of a IVa group element, Va group element, VIa group
element, Al, Si, Y, B, and S, and at least one type of element selected from the group
consisting of boron, carbon, nitrogen, and oxygen. The coat film preferably includes
one or more layers other than the first coat layer. The coat film preferably has an
entire thickness greater than or equal to 3 µm and less than or equal to 50 µm. The
first coat layer is preferably formed of alumina.
ADVANTAGEOUS EFFECTS OF INVENTION
[0015] The surface-coated cutting tool of the present invention allows both wear resistance
and chipping resistance to be highly established by the structure set forth above.
BRIEF DESCRIPTION OF DRAWINGS
[0016]
Fig. 1 is a schematic view of a surface-coated cutting tool and a workpiece material
in a contacting state during a cutting operation.
Fig. 2 is a schematic view of a surface-coated cutting tool having a rake face of
a square shape.
Fig. 3 is a schematic sectional view of a chamfer portion that is chamfered in a curve.
Fig. 4 is a schematic sectional view of a chamfer portion that is chamfered in a flat
plane.
Fig. 5 is a graph of residual stress distribution taking a minimal value at a depth
A of a first coat layer, and increasing continuously as a function of depth in the
depth direction from depth A.
Fig. 6 is a graph of residual stress distribution taking a minimal value at a depth
A of a first coat layer, and increasing stepwise as a function of depth in the depth
direction from depth A.
Fig. 7 is a schematic sectional view of a crystal structure of a first coat layer
in the proximity of the chamfer portion.
Fig. 8 is a schematic sectional view of a crystal structure of a first coat layer
in the proximity of the chamfer portion.
DESCRIPTION OF EMBODIMENTS
[0017] The present invention will be described in detail hereinafter. In the present invention,
it is assumed that the layer thickness or film thickness is measured using a scanning
electron microscope (SEM).
<Surface-Coated Cutting Tool>
[0018] The surface-coated cutting tool of the present invention includes a base material,
and a coat film formed thereon. The surface-coated cutting tool of the present invention
having this basic configuration is significantly useful as a drill, end mill, indexable
insert for drilling, indexable insert for end milling, indexable insert for milling,
indexable insert for lathing, metal saw, gear cutting tool, reamer, tap, and the like.
[0019] Fig. 1 is a schematic view of a surface-coated cutting tool and a workpiece material
in a contacting state during a cutting operation. A surface-coated cutting tool 1
of the present invention includes a rake face 2 brought into contact with a swarf
6 of workpiece material 5 in a cutting operation, and a flank face 3 in contact with
the workpiece material itself, as shown in Fig. 1. The ridge where rake face 2 and
flank face 3 meet is a chamfer portion 4 subjected to a cutting edge treatment. Chamfer
portion 4 is the region where surface-coated cutting tool 1 is brought into contact
with workpiece material 5, and particularly critical in the cutting tool.
[0020] Fig. 2 is schematic diagram of a surface-coated cutting tool having a square-shape
rake face 2. In the case where surface-coated cutting tool 1 of the present invention
is an indexable insert type cutting tool, a through hole 20 may be formed passing
through the top face and bottom face of rake face 2 at the middle of the indexable
insert cutting tool. This through hole 20 is used as a fixation hole for attaching
a tool. As necessary, another fixing means may be provided in addition to or alternative
to the fixation hole.
<Chamfer portion>
[0021] Fig. 3 is a schematic sectional view of a chamfer portion that is chamfered to have
a curved face. Fig. 4 is a schematic sectional view of a chamfer portion that is chamfered
to have a flat face. In the present invention, chamfer portion 4 implies a portion
that is chamfered (honing portion) at the region corresponding to the ridge where
rake face 2 and flank face 3 meet, subjected to a cutting edge treatment so as to
have a curve (R), as shown in Fig. 3, as well as a portion that is chamfered (negative
land portion) by linear cut off of the region corresponding to the ridge where rake
face 2 and flank face 3 meet, as shown in Fig. 4. Moreover, a portion based on a combination
of the above-described chamfered process is included.
[0022] Chamfer portion 4 is formed by subjecting the ridge where rake face 2 and flank face
3 meet to grinding, brushing, barreling treatment, blasting, buffing, honing, and
the like. When the surface-coated cutting tool is in plan view from the rake face
direction or flank face direction (Fig. 4), the width of chamfer portion 4 is preferably
greater than or equal to 0.01 mm and less than or equal to 0.2 mm, more preferably
greater than or equal to 0.02 mm and less than or equal to 0.1 mm.
<Base Material>
[0023] As the base material for the surface-coated cutting tool of the present invention,
any well-known base material for a cutting tool may be used without limitation. For
example, cemented carbide (for example, WC based cemented carbide, including Co in
addition to WC, or those further added with a carbon nitride such as Ti, Ta, Nb),
cermet (those with TiC, TiN, TiCN and the like as the main component), high-speed
steel, ceramics (titanium carbide, silicon carbide, silicon nitride, aluminum nitride,
aluminum oxide, a composite thereof, or the like), sintered cubic boron nitride, sintered
diamond, sintered boron nitride, or a composite formed of aluminum oxide and titanium
carbide can be cited as the base material.
[0024] Among the base materials set forth above, cemented carbide (WC based cemented carbide)
is preferable. This is because cemented carbide is an alloy having both hardness and
strength, having extremely favorable balance since cemented carbide contains iron
group metal such as cobalt with tungsten carbide of high hardness as the main component.
In the case where such cemented carbide is employed as the base material, the advantage
of the present invention can be exhibited even if the cemented carbide includes free
carbon or an abnormal phase called η phase in the texture.
[0025] The base material may have the surface modified. For example, in the case where cemented
carbide is employed, a β free layer may be formed at the surface. In the case where
cermet is employed, a surface harden layer may be formed. The advantage of the present
invention is exhibited even if the surface is modified.
<Coat Film>
[0026] In the surface-coated cutting tool of the present invention, the coat film formed
on the base material is characterized in including at least a first coat layer. The
coat film of the present invention may be formed by a first coat layer alone (in this
case, the first coat layer will be formed in contact with the base material), or include
one or more additional layer other than the first coat layer. This layer other than
the first coat layer may be formed between the base material and the first coat layer,
or on the first coat layer, as will be described afterwards. Even in the case where
the layer other than the first coat layer is formed on the first coat layer, the first
coat layer is the outermost layer (the layer constituting the surface of the coat
film) at the chamfer portion involved in cutting. By virtue of the first coat layer
including crystals having a different average grain size depending upon the site,
the first coat layer has residual stress suitable for that site. Thus, both wear resistance
and chipping resistance can be highly established. The grain size and residual stress
of the first coat layer will be described afterwards.
[0027] The coat film of the present invention includes the case where the entire face of
the base material is covered, the case where the coat film is provided only partially,
and also the case where the layering state of a portion of the coat film is partially
different. Preferably, the coat film of the present invention has an entire thickness
that is greater than or equal to 3 µm and less than or equal to 50 µm. If the thickness
is less than 3 µm, the wear resistance may be degraded. If the thickness exceeds 50
µm, the adherence with the base material as well as the chipping resistance may be
degraded. Particularly, the coat film has a thickness preferably greater than or equal
to 5 µm and less than or equal to 25 µm.
[0028] For the coat film of the present invention, the well-known coat film used for the
application set forth above can be used without particular limitation. The coat film
of the present invention is preferably formed of a compound including at least one
type of element selected from the group consisting of the IVa group element (Ti, Zr,
Hf, or the like), Va group element (V, Nb, Ta, or the like), VIa group element (Cr,
Mo, W, or the like) of the periodic table of elements, aluminum (Al), silicon (Si),
yttrium (Y), boron (B), and sulfur (S), and at least one type of element selected
from the group consisting of boron, carbon, nitride, and oxygen (excluding the case
where both elements are B). For the compound, a carbide, nitride, oxide, boride, carbonitride,
carbon oxide, oxynitride, carbon oxynitride, or the like of elements selected from
the group consisting of the aforementioned IVa group element (Ti, Zr, Hf, or the like),
Va group element (V, Nb, Ta, or the like), VIa group element (Cr, Mo, W, or the like),
aluminum (Al), silicon (Si), and yttrium (Y) can be cited. A solid solution thereof
may be included.
[0029] For the compound, a nitride, carbide, oxide, carbonitride, oxynitride, carbon oxynitride,
or the like of Ti, Al, (Ti
1-xAl
x), (Al
1-xZr
x), (Ti
1-xSi
x), (Al
1-xCr
x), (Ti
1-xySi
xAl
y) or (Al
1-x-yCr
xV
y) (also those including B, Cr or the like added thereto) can be cited as a suitable
composition (in the formula, x and y represent an arbitrary number equal to or less
than 1).
[0030] More preferably, TiCN, TiN, TiSiN, TiSiCN, TiAlN, TiAlCrN, TiAlSiN, TiAlSiCrN, AlCrN,
AlCrCN, AlCrVN, TiBN, TiAlBN, TiBCN, TiAlBCN, TiSiBCN, AlN, AlCN, AlO, Al
2O
3, ZrO
2, (AlZr)
2O
3, and the like can be cited. The first coat layer constituting the coat film will
be described in further detail hereinafter.
<Residual Stress of First Coat Layer>
[0031] In the first coat layer of the present invention, the residual stress thereof greatly
differs according to the depth of the chamfer portion as well as between the chamfer
portion and a portion other than the chamfer portion, and satisfies all the conditions
of (1)-(5) set forth below.
- (1) The first coat layer at the chamfer portion has residual stress exhibiting a minimal
value at a depth A that is within 2 µm from the surface.
- (2) The minimal value of the aforementioned residual stress is greater than or equal
to -7 GPa and less than or equal to -1 GPa.
- (3) The residual stress increases continuously or stepwise as a function of depth
further in the depth direction from depth A.
- (4) A portion of the first coat layer other than the chamfer portion has residual
stress greater than the minimal value of the residual stress of the chamfer portion
in the first coat layer.
- (5) A portion of the first coat layer other than the chamfer portion has residual
stress increasing continuously or stepwise as a function of advancing towards the
central direction of the rake face and the central direction of the flank face, and
greater than or equal to 0 GPa and less than or equal 2 GPa at the base material side.
[0032] An example of the stress distribution in the first coat layer satisfying the conditions
of (1)-(3) among (1)-(5) set forth above is shown in Figs. 5 and 6. Fig. 5 is a graph
representing a stress distribution in which the minimal value is exhibited at depth
A of the first coat film, and the residual stress increases continuously as a function
of depth in the depth direction from said depth A. Fig. 6 is a graph similar to that
of Fig. 5, provided that the increase of the residual stress is stepwise.
[0033] By virtue of the first coat layer of the present invention having such a stress distribution
together with the crystal structure of the first coat layer that will be described
afterwards, both the wear resistance and chipping resistance are highly established.
In addition, the adherence between the base material and the coat film is further
improved. By the minimal residual stress in the proximity of the surface of the coat
film (first coat layer), development of a crack generated at the surface of the coat
film during cutting can be suppressed. The conditions of (1)-(5) and resulting advantage
will be described hereinafter.
[0034] By satisfying the condition of (1), the balance between wear resistance and chipping
resistance can be maintained. Depth A where the residual stress is minimal is preferably
located in the range greater than or equal to 0.1 µm and less than or equal to 1 µm
from the surface of the first coat layer. If depth A exceeds 2 µm from the surface
of the first coat layer, the balance between the wear resistance and chipping resistance
is lost, which may degrade the tool lifetime.
[0035] By satisfying the condition of (2), a surface-coated cutting tool less susceptible
to self destruction at the coat film during cutting, and superior in chipping resistance
can be obtained. The minimal value of the residual stress is preferably greater than
or equal to -5 GPa and less than or equal to -1.5 GPa. If the minimal value of the
residual stress is less than -7 GPa, the compressive stress of the first coat film
will be so high that self destruction will occur to facilitate chipping. If the minimal
value exceeds -1 GPa, the chipping resistance required for a cutting tool cannot be
achieved. As used herein, "minimal value" in the present invention implies the smallest
value in numeric meaning, as well as the case where the residual stress indicates
a constant numeric value continuously in the thickness direction of the first coat
layer, as shown in Fig. 8 described afterwards.
[0036] The condition of (3) is provided for the purpose of excluding the case where the
residual stress includes any locally high or low value. In the case where the residual
stress is locally high or low, chipping will readily occur with that region as the
origin. Such occurrence of chipping can be suppressed by satisfying the present condition
(3) (variation of the residual stress in a continuous or stepped manner).
[0037] By satisfying the conditions of (4) and (5), the residual stress gradually increases
(compressive stress also gradually reduces) towards the central direction of the rake
face or flank face of the first coat layer. Accordingly, internal destruction of the
coat film by its own stress can be prevented. The portion of the first coat layer
other than the chamfer portion preferably has residual stress that is eventually greater
than or equal to 0 GPa and less than or equal to 2 GPa. Exceeding the residual stress
of 2 GPa at a portion of the first coat layer other than the chamfer portion is not
preferable since the coat film will peel off at the chamfer portion depending upon
the shape of the cutting tool. If the residual stress at the aforementioned base material
side is less than 0 GPa, sufficient wear resistance cannot be achieved.
[0038] As used herein, "central direction of the rake face" implies the vector direction
towards the center of the rake face from any one point of the ridge of the cutting
edge that is the chamfer portion. Similarly, "central direction of the flank face"
implies the vector direction towards the center of the flank face from any one point
of the ridge of the cutting edge that is the chamfer portion.
[0039] As used herein, compressive stress in the present invention refers to a type of the
internal stress present in the coat film (inherence strain) represented by a "-" (minus)
numeric value (unit:GPa). Therefore, high compressive stress (internal stress) means
that the absolute value of the aforementioned numeric value becomes larger whereas
a low compressive stress (internal stress) means that the absolute value of the above-described
numeric value becomes smaller. It is to be noted that a numeric value represented
with "+" (plus) refers to the tensile stress.
[0041] In the present invention, first the penetration depth of the X-ray is fixed by a
combination of the ISO-inclination method and side inclination method. The diffraction
angle 2θ relative to various ϕ directions in the plane including the measuring stress
direction and the normal of the specimen surface at the position of measurement is
measured to produce a 2θ - sin
2ϕ line map. From the gradient, the compressive stress up to the relevant depth (distance
from the surface of the coat film) is obtained.
[0042] More specifically, in the X-ray stress measurement method, an X-ray from an X-ray
source is directed to the first coat layer at a predetermined angle. The X-ray diffracted
at the first coat layer is detected with an X-ray detector. The internal stress is
measured based on the detected value.
[0043] As an X-ray source for the measurement of the residual stress in the thickness direction
of the coat film, synchrotron radiation (SR) is preferably used from the standpoint
of the property of the X-ray source (high luminance, high degree of parallelization,
variable wavelength, and the like).
[0044] In order to obtain the above-described compressive stress from a 2θ - sin
2ϕ line map, the Young's modulus and Poisson's ratio of the coat film are preferably
used. The Young's modulus can be measured using a dynamic hardness tester. For the
Poisson's ratio, a value in the vicinity of 0.2 should be used since it does not vary
greatly by the material. When the compressive stress is to be obtained from the 2θ
- sin
2ϕ line map, the Young's modulus does not necessarily have to be used. The compressive
stress may be calculated using the lattice constant and lattice spacing instead.
<Composition of First Coat Layer>
[0045] Preferably, the first coat layer is formed of a compound including at least one type
of element selected from the group consisting of the IVa group element (Ti, Zr, Hf,
or the like), Va group element (V, Nb, Ta, or the like), VIa group element (Cr, Mo,
W, or the like) of the periodic table of elements, aluminum (Al), silicon (Si), yttrium
(Y), boron (B), and sulfur (S), and at least one type of element selected from the
group consisting of boron, carbon, nitride, and oxygen (excluding the case where both
elements are B), more preferably formed of alumina, and further preferably formed
of alumina having an α type crystal structure
<Crystal Structure of First Coat Layer>
[0046] Figs. 7 and 8 are schematic sectional views of the crystal structure of the first
coat layer in the neighborhood of the chamfer portion. Figs. 7 and 8 represent the
case where the coat film includes a first coat layer alone. First coat layer 8 of
the present invention includes a fine crystal texture region 10 where the average
grain size of the constituent compound is small and a rough crystal texture region
9 where the average grain size is large. The first coat layer is formed by the aggregation
of compound crystal grains. The region where crystal grains having an average grain
size of 10-200 nm aggregate is referred to as the fine crystal texture region, whereas
the region where crystal grains larger than the crystal in the fine crystal texture
region is referred to as the rough crystal texture region.
[0047] The fine crystal texture region constitutes the region up to a depth A from the surface
of first coat layer 8 at chamfer portion 4, as shown in Figs. 7 and 8. Specifically,
first coat layer 8 at chamfer portion 4 is formed of two regions in the thickness
direction, i.e. rough crystal texture region 9 at the side of base material 7 and
fine crystal texture region 10 at the surface side. The thickness of fine crystal
texture region 10 constitutes the region from the surface of first coat layer 8 up
to depth A.
[0048] The present invention allows both wear resistance and chipping resistance to be highly
established by virtue of first coat layer 8 taking the configuration set forth above.
Specifically, the formation of fine crystal texture region 10 at the surface of first
coat layer 8 reduces the unit of destruction of the coat film, leading to improvement
in wear resistance. Moreover, the grain boundary increases by miniaturizing the crystal
grains. Accordingly, a crack generated at the coat film surface side will not develop
towards the base material side, leading to improvement in chipping resistance. Furthermore,
the provision of an interface differing in grain size in the coat film suppresses
the development of a crack at the interface between the fine crystal texture region
and rough crystal texture region. Furthermore, improvement in toughness can be expected.
The reason why large crystal grains are aggregated at the base material side is to
improve the adherence between first coat layer 8 and base material 7 by the growth
of the crystals in first coat layer 8 following the crystals constituting base material
7. Thus, first coat layer 8 of the present invention functions to highly establish
both wear resistance and chipping resistance as well as to improve the adherence with
base material 7.
[0049] In order to achieve the effect set forth above, the average grain size of the crystal
grains in the fine crystal texture region must be greater than or equal to 10 nm and
less than or equal to 200 nm, more preferably greater than or equal to 15 nm and less
than or equal to 80 nm. If the grain size is less than 10 nm, the wear resistance
will be degraded since the binding between grains constituting the crystal texture
of first coat layer 8 will become weaker. If the average grain size exceeds 200 nm,
the crystal texture of the coat film at the cutting surface will be so rough that
adhesive wear occurs on the workpiece material, leading to degradation in the wear
resistance.
[0050] Although the average grain size of the crystal grains in the rough crystal texture
region has a different optimum range depending upon the average grain size of the
crystal grains in the fine crystal texture region, the crystal grain size of the rough
crystal texture region is basically greater than the crystal grain size of the crystal
grains in the fine crystal texture region, and is preferably greater than or equal
to 200 nm, more preferably greater than or equal to 300 nm and less than or equal
to 1500 nm.
[0051] The average grain size of the crystal grains in the present invention can be obtained
as set forth below. The base material and the coat film (first coat layer) formed
on the base material are treated such that the cross section is visible with an FIB
worked material. The cross section is observed with an FE-SEM (Field Emission-Scanning
Electron Microscope). Through an observance as a reflected electron image, the portion
having the same crystal orientation is observed at the same contrast. The portion
of the same contrast is taken as one crystal grain.
[0052] Then, with respect to the obtained image, a straight line of an arbitrary length
(preferably, around 400 µm) is drawn parallel to the surface of the base material
at an arbitrary site of the first coat layer. The number of crystal grains included
in the straight line is measured. The length of the straight line is divided by the
number of crystal grains. The value thereof is taken as the average grain size at
that site of the first coat layer.
[0053] The interface between the fine crystal texture region and rough crystal texture region
is taken as the location where the orientation of the crystal in a direction perpendicular
to the surface of the base material changes, based on the observance of the cross
section of the coat film (first coat layer) using a transmission type electron microscope.
Alternatively, in the case where a definite change based on the boundary of the site
having such crystal orientation is not shown and the orientation changes with a certain
width (the length in the direction perpendicular to the surface of the base material),
the middle point of that width is taken as the interface between the fine crystal
texture region and rough crystal texture region.
<Position of First Coat Layer>
[0054] In the case where the coat film is formed of a plurality of layers in the present
invention, the first coat layer may be formed at the base material side or surface
side of the coat film. Preferably, the first coat layer is located at the outermost
surface layer. Accordingly, the first coat layer will be brought into contact with
the workpiece material, suppressing any loss at the initial stage of cutting. The
cutting performance can be improved and the lifetime increased. At the chamfer portion,
the first coat layer is necessarily the outermost surface layer of the coat film.
<Thickness of First Coat Layer>
[0055] In the present invention, the first coat layer has a thickness preferably greater
than or equal to 2 µm and less than or equal to 30 µm. Moreover, the upper limit of
thickness is 20 µm, more preferably 10 µm. The lower limit of the thickness is 3 µm,
more preferably 5 µm. If the thickness is less than 2 µm, the effect in improving
the chipping resistance is not so appreciable since the effect of the residual compressive
stress, when applied, is not sufficient. If the thickness exceeds 30 µm, the adherence
with the base material or the layer located at the inner side of first coat layer
may be degraded.
<Additional Layer Other than the First Coat Layer>
[0056] The coat film of the present invention may include one or more additional layer other
than the above-described first coat layer. Such a layer includes an intermediate layer
formed between the base material and the first coat layer, and/or the outermost surface
layer formed on the first coat layer. These layers are provided for the purpose of
anti-oxidation, lubrication, and the like, relative to the above-described effects
of the first coat layer.
[0057] Particularly, the aforementioned intermediate layer is provided for the purpose of
improving wear resistance and/or adherence with the base material. The intermediate
layer may include one or more layers. The intermediate layer may be formed of, for
example, TiC, TiN, TiCN, TiCNO, TiSiN, TiAlN, TiZrCN, TiAlCrN, TiAlSiN, TiAlCrSiN
and the like. In these compositions, the ratio of respective atoms is not particularly
limited, and follows the conventionally well known ratio. The intermediate layer is
formed preferably to have a thickness greater than or equal to 0.2 µm and less than
or equal to 1 µm, and residual stress greater than or equal to -1 GPa and less than
or equal to -0.1 GPa.
[0058] The outermost surface layer is formed for the purpose of coloring or the like to
identify a used cutting edge, and may include one or more layers. The outermost surface
layer is formed of, for example Cr, CrN, TiN , TiCN, or the like. In these compositions,
the ratio of respective atoms is not particularly limited, and follows the conventionally
well known ratio. The outermost surface layer is preferably formed to have a thickness
greater than or equal to 0.1 µm and less than or equal to 0.3 µm.
<Production Method>
[0059] The chamfer portion is formed by subjecting the ridge where the rake face and the
flank face of the base material meet to grinding, brushing, barreling treatment, milling,
and the like. A coat film is deposited on the base material with the chamfer portion
formed.
[0060] For the method of producing a coat film of the present invention, the well known
conventional method can be used without particular limitation. Preferably, the coat
film is formed by chemical vapor deposition. Forming a coat film by CVD is advantageous
in that each layer of the coat film has residual tensile stress, exhibiting high adherence
with the base material.
[0061] The formed coat film is characterized in that the chamfer portion of the first coat
layer is subjected to blasting locally. Accordingly, compressive stress can be applied
to the chamfer portion at the surface side of the first coat layer, and the average
grain size of the crystal grains located up to depth A from the surface of the first
coat layer at the chamfer portion is reduced to be greater than or equal to 10 nm
and less than or equal to 200 nm.
[0062] Blasting is carried out by preparing a dispersing solvent having abrasive grains
dispersed directly or into a solvent such as of water, and causing the dispersing
solvent to collide against the surface of the first coat layer. In the present invention,
blasting is carried out with the volume ratio of the grains in the dispersing solvent
varied in the range greater than or equal to 5 volume % and less than or equal to
40 volume % while gradually thinning the abrasive grain concentration by increasing
the concentration of the liquid in the dispersing solvent continuously or stepwise.
The abrasive grains are preferably based on a mixture of at least two types of powder
differing in specific gravity and hardness. For example, a mixture of two types of
powder, i.e. powder of diamond, boron nitride, silicon carbide, or the like of high
hardness and low specific gravity, and powder such as of zirconia, tantalum carbide,
tungsten carbide, or the like having low hardness and high specific gravity is preferably
used. Furthermore, the blast treatment may be divided into two stages, using different
powder at each step.
[0063] The collision condition of the abrasive grains may be adjusted appropriately depending
upon the configuration of the coat film and/or the level of the applied residual compressive
stress. Preferably, the pressure projection is greater than or equal to 0.01 MPa and
less than or equal to 0.5 MPa; the projection distance is greater than or equal to
0.5 mm and less than or equal to 50 mm; and the projection angle is at right angle
to the chamfer portion. If the collision strength of the grains is not sufficient,
the desired residual compressive stress cannot be applied. It is therefore preferable
to apply collision at an appropriate strength.
[0064] Although the present invention is characterized in that the residual stress and grain
size of the first coat layer at the chamfer portion are altered by blasting set forth
above, the case where a portion of the first coat layer other than the chamber portion
has residual stress and grain size equal to the region of the first coat layer at
the chamfer portion and the case where the residual stress and grain size set forth
above are partially satisfied at the chamfer portion of the first coat layer are included
in the scope of the present invention as long as the advantage of the present invention
is not degraded.
EXAMPLES
[0065] Although the present invention will be described in further detail based on examples,
the present invention will not be limited thereto. The compound composition of the
coat films in the examples and comparative examples were confirmed by an X-ray photoelectron
spectrometer (XPS).
[0066] Raw material powder based on the blend of 86 mass % of WC, 8.0 mass % of Co, 2.0
mass % of TiC, 2.0 mass % of NbC, and 2.0 mass % of ZrC was mixed for 72 hours using
a bowl mill. Then, the mixture was dried, press-formed, and subjected to sintering
for 1 hour at the temperature of 1420°C in a vacuum atmosphere to produce the base
material for a throwaway tip made of WC based cemented carbide (shape:Sumitomo Electric
Hardmetal Corp., CNMG120408).
[0067] The cutting edge of such base material was subjected to chamfering by means of a
nylon brush including SiC abrasive grains to form a round honing as the chamfer portion.
Then, the surface of the base material was cleaned.
[0068] By means of the well-known thermal CVD method, each layer of the coat film shown
in the column of "Layer Structure" in Table 1 was formed on the base material (the
layer of the composition from the right side indicated in the column of "layer structure"
in Table 1 was formed on the base material in the cited order). For example, Example
3 had a TiN layer or 0.3 µm in thickness, a TiCN layer of 10 µm in thickness, then
a TiCNO layer of 0.5 µm in thickness, and a κ-Al
2O
3 layer of 4 µm in thickness formed in the cited order from the base material side.
The first coat layer in each example is the outermost surface layer.
[0069] The chamfer portion of the first coat layer was subjected to blasting using zirconia
having a hardness lower than and a specific gravity greater than the coat film, and
diamond abrasive grains of high hardness and low specific gravity. Specifically, the
abrasive grain concentration was gradually thinned while the concentration of the
liquid was increased continuously or stepwise and adjusting the projection distance
of 0.5-50 mm at the projection pressure of 0.01-0.5 MPa to subject the chamfer portion
of the coat film to blasting. Thus, the first coat layer was treated by two types
of media to attain the residual stress and fine texture indicated in Table 1 below.
The "Increasing Manner" column in Table 1 indicates whether the increasing manner
of the residual stress was "continuously" or "stepwise". In the comparative example,
"constant" in the corresponding column implies that the increasing manner of the residual
stress at the first coat layer was constant.
[0070] The surface-coated cutting tool in each of examples was fabricated by a similar way.
The surface-coated cutting tool in each of the comparative examples was produced according
to a method similar to that of each of the examples set forth above, provided that
the above-described blasting was not carried out.
[0071] The distribution of the residual stress at the first coat layer was measured by the
sin
2ϕ method for the produced surface-coated cutting tool. The average grain size of the
first coat layer was based on observing the cross section of the coat film according
to the method set forth above.
[0072] In the measurement by the sin
2ϕ method, the energy of the employed X-ray was 10 keV, and the peak of the diffraction
line was the (166) plane of α type Al
2O
3. The measured diffraction peak position was determined by the fitting of the Gauss
function. The inclination of the 2θ-sin
2ϕ line graph was obtained. For the Young's modulus, the value obtained using a dynamic
hardness tester (MST-made nanoindenter) was used. For the Poisson ratio, the value
of Al
2O
3 (0.2) was used.

[0073] In the column of "Film Thickness" for each layer in Table 1, the thickness of each
layer constituting the coat film was indicated in the parenthesis at the side of each
layer in Table 1. The film thickness and layer thickness were obtained by cutting
at a plane including the normal to the surface of the surface-coated cutting tool,
and using relevant values based on an observation of the cut face by an SEM.
[0074] In Table 1, the column "Depth A" indicates the distance where the residual stress
becomes minimal from the surface of the first coat layer. The minimal value of the
relevant residual stress is indicated in the column of "Minimal Value" in Table 1.
The column of "Increasing Manner" indicates whether the increasing manner of the residual
stress towards the central direction of the rake face and flank face is "continuous"
or "stepwise".
[0075] The column of "Fine" in "Average Grain Size" represents the average grain size of
the crystal grains from the surface of the first coat layer down to depth A at the
chamfer portion(fine crystal texture region). The column of "Rough" represents the
average grain size of the crystal grains at a portion of the first coat layer other
than the fine crystal texture region.
<Cutting Specimen>
[0076] Using the surface-coated cutting tool of each example and each comparative example,
a lathe turning cutting test was carried out in accordance with the conditions set
forth below.
Workpiece material : |
FCD700 round rod with a groove |
Cutting speed : |
230 m/min |
Feed rate : |
0.15 mm/rev |
Cut : |
1.0 mm |
Cutting oil : |
used |
[0077] The time before chipping was generated at the surface-coated cutting tool from the
start of the cutting test is shown in the column of "Chipping Occurring Time" in Table
2. A longer chipping occurring time implies that chipping does not readily occur at
the cutting tool.
[0078] By measuring the surface-coated cutting tool with the vernier caliper for every one
minute from the start of the cutting test, the width of the reduction by wear at the
flank face was calculated, and the time until this width exceeded 0.25 mm in average
is indicated in the column of "Tool Lifetime" in Table 2. A longer tool lifetime implies
that the lifetime of the surface-coated cutting tool is longer.
Table 2
|
Chipping Occurring Time (min) |
Tool Lifetime (min) |
Example |
1 |
21 |
55 |
2 |
20 |
53 |
3 |
42 |
78 |
4 |
32 |
81 |
5 |
35 |
101 |
6 |
22 |
88 |
7 |
18 |
92 |
Comparative Example |
1 |
2 |
10 |
2 |
3 |
20 |
3 |
8 |
25 |
4 |
5 |
26 |
5 |
1 |
18 |
[0079] It is apparent from the results in Table 2 that the surface-coated cutting tool of
each example of the present invention has a small wear amount at the flank face and
chipping does not readily occur, as compared to those of the comparative example.
From these results, it can be said that the surface-coated cutting tool of each example
of the present invention is superior in wear resistance and chipping resistance, as
compared to those in each of the comparative examples. The reason why the wear resistance
and chipping resistance of the surface-coated cutting tool in each of the examples
set forth above are improved is due to miniaturizing the crystals at the chamfer portion
of the first coat layer and locally reducing the residual stress at that portion.
[0080] From the above results, it was identified that the surface-coated cutting tool of
the examples were superior in wear resistance and chipping resistance, as compared
to the surface-coated cutting tool of the comparative examples.
[0081] Although the present invention has been described based on embodiments and examples
as set forth above, it is intended that the features of the embodiments and examples
may be combined appropriately.
[0082] Furthermore, it should be understood that the embodiments and examples disclosed
herein are illustrative and nonrestrictive in every respect. The scope of the present
invention is defined by the terms of the claims, rather than description set forth
above, and is intended to include any modification within the scope and meaning equivalent
to the terms of the claims.
REFERENCE SIGNS LIST
[0083] 1 surface-coated cutting tool; 2 rake face; 3 flank face; 4 chamfer portion; 5 workpiece
material; 6 swarf; 7 base material; 8 first coat layer; 9 rough crystal texture region;
10 fine crystal texture region; 20 through hole.